Takano, A.; Yoshino, K.; Fukushima, Y.; Kitamura, R.; Funami, Y.; Takahashi, K.; Takahashi, A.; Kunihiro, Y.; Miyake, M.; Masai, T.;
et al. System Design and Launch of a Hybrid Rocket with a Star-Fractal Swirl Fuel Grain Toward an Altitude of 15 km. Appl. Sci. 2024, 14, 11297.
https://doi.org/10.3390/app142311297
AMA Style
Takano A, Yoshino K, Fukushima Y, Kitamura R, Funami Y, Takahashi K, Takahashi A, Kunihiro Y, Miyake M, Masai T,
et al. System Design and Launch of a Hybrid Rocket with a Star-Fractal Swirl Fuel Grain Toward an Altitude of 15 km. Applied Sciences. 2024; 14(23):11297.
https://doi.org/10.3390/app142311297
Chicago/Turabian Style
Takano, Atsushi, Keita Yoshino, Yuki Fukushima, Ryuta Kitamura, Yuki Funami, Kenichi Takahashi, Akiyo Takahashi, Yoshihiko Kunihiro, Makoto Miyake, Takuma Masai,
and et al. 2024. "System Design and Launch of a Hybrid Rocket with a Star-Fractal Swirl Fuel Grain Toward an Altitude of 15 km" Applied Sciences 14, no. 23: 11297.
https://doi.org/10.3390/app142311297
APA Style
Takano, A., Yoshino, K., Fukushima, Y., Kitamura, R., Funami, Y., Takahashi, K., Takahashi, A., Kunihiro, Y., Miyake, M., Masai, T., & Uemura, S.
(2024). System Design and Launch of a Hybrid Rocket with a Star-Fractal Swirl Fuel Grain Toward an Altitude of 15 km. Applied Sciences, 14(23), 11297.
https://doi.org/10.3390/app142311297
